Gee Rob, and here I thought my biplane reference would put you off the trail to correct answers! Congratulations, Again!
Here are mine.
1. Sweden
2a. 1952. 2b. Viggen System 37 air defense network (airborne component of). 2c. SAAB
3a. AJ 37 Viggen. 3b. SF 37, SH 37, SK 37 (two seats), final production JA 37.
4a. Feb. 8, 1967. 4b. 2007.
5. The SAAB Lassen and the SAAB Draken.
6. This question admittedly not well posed. My apologies. The final JA 37 Viggen version used one modified Volvo Flygmotor RM8B Turbofan with after-burning which was a license-built adaptation of the P&W JT8D with the USA providing advanced engine technology agreements. Early Viggens used the modified Volvo RM8A version of the JT8D with less power.
The Viggen (Thunderbolt or Tufted Duck) depending on interpretation of the word Viggen, was an advanced for its time aircraft used for many roles-air superiority, close air support, reconnaissance, and maritime surveillance for over 30 years in service. Requirements were: supersonic low altitude flight, Mach 2 high-altitude flight, unprecedented STOL capability including operation on primitive roadways and to be simple to service by inexperienced ground crews. Early versions were dangerous with 40 lost of total of all versions-149 built.
To meet these extreme requirements the Viggen design had a then-unconventional delta-wing configuration with two-section elevons, foreplane fixed-canard with trailing-edge flaps, tandem main wheel tri-gear. Thrust reversers and the tandem undercarriage allowed short, non-flare landings after early landing problems on damaged runways/roads-(a design requirement). Early version was underpowered, hence the RM8B version engine. The last operation date I have for the Viggen is 2007. Swedish policy: No foreign sales.
Specs for JA 37 Viggen
Power: one Volvo RM8B turbofan 16,203 lb thrust, with afterburning 28,108 lb thrust.
Max speed: at altitude above Mach 2,or more than 1,145 kts, at 330' max speed Mach 1.2
Cruise speed: 600 mph
Time to climb to 32,800'-less than 1 min, 42 sec.
Weight loaded: 37,348 lb
Max range: 1,200 miles with internal fuel
Wingspan: 34'9"
Length overall with probe: 53'10" Fuselage: 51'2"
Height: 19'4"
Wing area: 495.1 sq ft
Armament
One 30mm Oerlikon KCA-cannon
Either six AIM-9 Sidewinders or two RB71 Skyflash and four AIM-120 AMRAAMs or four rockets.